Climb analyzed, including effects of tangential accelerations; three flight performances examined: minimum time of climb, climb with minimum fuel consumption, and steepest climb. Bibliography. English translation from Aerotecnica 1952.
Optimum flight paths of turbojet aircraft
NACA -- Tech Memo
National Advisory Committee for Aeronautics -- Technical Memorandums ; 32 , Memo 1389, n 4
1955
47 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Optimum flight paths of turbojet aircraft
NTRS | 1955
|Approximate solutions to optimum flight trajectories for turbojet-powered aircraft
Engineering Index Backfile | 1959
|Aircraft Optimum Multiple Flight Paths
NTIS | 1970
|Aerodynamics and Flight Dynamics of Turbojet Aircraft
NTIS | 1969
|